M.D. Sensmeier and J.A. Samareh, A study of vehicle structural layouts in post-WWII aircraft, 45th AIAA/ASME/ASCE/AHS /ASC Structures, Structural Dynamics & Materials Conference, Palm Springs, California, 2004.
Hu Tianyuan and Yu Xiongqin, Aerodynamic/ Stealthy/ Structural Multidisciplinary Design Optimization of Unmanned Combat Air vehicle, Chinese Journal of Aeronautics, 16 September 2008.
Wolf R. Krüger, D. Hoffmann, Design Considerations for a UCAV Wing for Subsonic and Transonic Aeroelastic and Flight Mechanic Wind Tunnel Tests, Meeting proceedings RTOMP-AVT-145, France, 2007.
 Hu Tianyuan, Aerodynamic / Stealthy / Structural Multidisciplinary Design Optimization of Unmanned Combat Air Vehicle, Chinese Journal of Aeronautics pp. 380-386, 2009.
 Yalin Pan, Application of Multidisciplinary Design Optimization on Advanced Configuration Aircraft, J. Aerosp. Technol. Manag., São José dos Campos, Vol.9, No 1, pp.63-70, Jan-Mar, 2017.
 P. N. Vinay, Investigation On Structural Aspects Of Unmanned Combat Air Vehicle For Aeroelastic Analysis, IJAET, Vol.II, Issue IV, October-December,2011/278-283.
 Evren Sakarya, A Study on Evaluation of Aeroelastic Characteristics of a UCAV Configuration, AIAA 10.2514/6.2018-3328, 2018.
 Johannes M. Schweiger, Atlee M. Cunningham Jr, Structural Design Efforts for the MULDICON Configuration, AIAA AVIATION Forum, June 25-29, 2018.
 J. Eves, et al, Topology Optimization of Aircraft with Non-Conventional Configurations, 8th World Congress on Structural and Multidisciplinary Optimization, June 1 - 5, Lisbon, Portugal, 2009.
 M. Johansson, Propulsion integration in an UAV, AIAA 2006–2834, 24th Applied Aerodynamics Conference, Reston, Virginia, US,5–8 June 2006.
 Shi, L. and R.W. Guo, Serpentine inlet design and analysis, AIAA 2012-0839, 50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition, Reston, Virginia, US, 9–12 January 2012.
 J. Whittenbury, Configuration design development of the navy UCAS-D X-47B, AIAA 2011–7041, AIAA Centennial of Naval Aviation Forum ‘100 Years of Achievement and Progress’, Reston, Virginia, US, 21–22 September 2011.
 Joe Coppin, Aerodynamics, Stability and Shape Optimization of Unmanned Combat Air Vehicles, PHD Thesis, University of Sheffield, Department of Mechanical Engineering, 2014.
 E. Sepulveda, H. Smith, Technology challenges of stealth unmanned combat aerial vehicles, The Aeronautical Journal September, Volume 121, No 1243, 2017.
 Leland M. Nicolai, Grant E.Carichner, Fundamentals of aircraft and airship design, Volume-I Aircraft Design, American institute of aeronautics and astronautics Inc., Restone, Virginia, 2010.
 Martin Neubauer, Structural Design Aspects and Criteria for Military UAV, Accessed on 8 July 2020; http://www.rto.nato.int/abstracts.asp.
 Maj. MERCURIO Andrea, nEUROn UCAV: Development and Operational Assessment Campaign, STO-MP-SCI-269, 2015.
 J. A.Samareh, Survey of Shape Parameterization Techniques for High-Fidelity Multidisciplinary Shape Optimization, AIAA Journal, Vol. 39, No. 5, pp. 877-883, 2001.
 Yu Wang, Lei Liu, Yu Xing, Zhenbo Yang, Investigation of wing structure layout of aerospace plane based on the finite element method, Advances in Mechanical Engineering, Vol. 9(7) 1–9, 2017.
 CATIA V5R19: User’s manual, CAD design, 2006.
 V. Saran, V. Jayakumar, G. Bharathiraja, Analysis of natural frequency for an aircraft wing structure under pre-stress, International Journal of Mechanical Engineering and Technology (IJMET), Volume 8, Issue 8, pp. 1118–1123,, August 2017.
 Yu Li, Jingwu He, Yuexi Xiong, Layout Design Optimization of Spars under Multiple Load Cases of the High-Aspect-Ratio Wing, International Journal of Aerospace and Mechanical Engineering Vol. 11, No:10, 2017.
 Gürkan İRSEL, stress analysis and design optimization with catia, Applied Computer Science, vol. 12, no. 1, pp. 27–39, 2015.
 Metallic materials and elements for aerospace vehicle structur, MIL-HDBK-5J, 31 january 2003, Accessed on 8 July 2020; http://www.everyspec.com.
 Chapman, R.E. Unmanned combat aerial vehicles: Dawn of a new age?, Air and Space Power J, 16, (2), pp 60-73, 2002.
 S. J. Woolvin, A conceptual Design Study of the 1303 configuration, 24th Applied Aerodynamics Conference, AIAA Paper 2006-2991, 2006.
 Carsten M., Russell M.Cummingsb, Andreas Schüttea, Jan Vormwega, Ryan G.Mayec, Tiger L.Jeansc, Multi-disciplinary design and performance assessment of effective, agile NATO air vehicles, Aerospace Science and Technology, DOI 10.1016/j.ast.2020.105764, 2020.
 C. M. ,Liersch, Gavin Bishop, Conceptual Design of a 53deg Swept Flying Wing UCAV Configuration, AIAA AVIATION Forum, Atlanta, Georgia, June 25-29, 2018.
 Arne Voss, Thomas Klimmek, Design and Sizing on a Parametric Structural Model for a UCAV Configuration for Loads and Aeroelastic Analysis, CEAS Aeronautical Journal, DOI 10.1007/s13272-016-0223-2, 2016.
 A. Levy, et al, Final Report, Project 7–8: Team Cerberus – UCAV, Haifa, Israel, 2009.
 E.A. Valencia, Weight assessment for a blended wing Body-Unmanned aerial vehicle implementing boundary layer ingestion, CMSME 2018.
 MSC/PATRAN Version 2012: User’s manual.
 HESA Material Test Results.